• 항공우주기술
• /
• 제4권1호
• /
• pp.143-149
• /
• 2005

로켓엔진용 연료펌프의 수력 성능과 흡입 성능을 관찰하기 위해 연료펌프에 대한 성능시험을 실시하였다. 성능 시험은 수력 성능 시험과 흡입 성능으로 나뉘며 시험의 편의를 위해 상온의 물을 매질로 택하였다. 수력 성능 시험 결과 양정, 효율, 볼류트 압력 분포 등은 상사 법칙을 잘 만족하는 것으로 드러났으나, 이차 유로의 압력 분포는 상사 법칙과 약간의 차이를 보였다. 그리고 플로팅 링 간극을 줄였을 때 펌프의 양정과 효율 모두 좋아지는 것을 확인할 수 있었고, 바이패스 배관의 오리피스 변화는 연료펌프의 효율 변화와 특별한 경향성을 보이지 않았다. 마지막으로 흡입 성능 시험 결과 펌프의 시험 회전수를 높였을 때 펌프의 흡입 성능이 증가하는 것을 관찰할 수 있었다.

• 한국생산제조학회지
• /
• 제22권3호
• /
• pp.465-471
• /
• 2013

Flow rate control is the uppermost concern for a trochoid hydraulic pump. Cavitation within the flow field of the pump has the greatest effect on the flow control during high-speed pump rotation of approximately 3500~4000 RPM. In this paper, based on AMESim$^{(R)}$ and Solid Works$^{(R)}$, we will present a method to simulate cavitation by analyzing the control factors of a trochoid pump, including the hydraulic pressure change at the outlet, flow rate based on the rotation speed of the inner rotor, leakage through the gap between the outer and inner rotors, and discharging angle of the outlet. The proposed methodology of the [cavitation simulation will enable field engineers to more easily design trochoid pumps, and will allow more concrete control over the flow rate of the pump by realizing an analysis model similar to the actual product model.

• 한국산학기술학회논문지
• /
• 제16권1호
• /
• pp.50-55
• /
• 2015

본 연구에서는 공동 주택의 수전 개방 조건에서, 감압밸브 내부 오리피스 형상이 캐비테이션 발생에 미치는 영향에 대하여 살펴보았다. 이를 위하여 감압밸브 내부의 유로형상을 9가지 유형으로 구별하여 제시하고, 3차원 유한해석 코드인 ANSYS CFX를 사용하여 감압밸브 내의 유동해석을 수행하였다. 급격한 단면 변화가 일어나는 오리피스에서 최저 압력과 최대 속도가 발생하였다. 최대속도가 존재하는 부위에서 0 이상 증기체적비를 나타내어 캐비테이션이 발생함을 확인하였다. 유로 길이가 긴 형상에 비하여 돌연 확대관 형상의 모델에서 유체의 최대 속도가 낮게 나타났다. 돌연확대관 형상의 경우에는 매우 작은 증기체적비를 나타내고 있으며, 돌연확대의 정도가 클수록 증기체적비는 낮게 나타났다. 따라서 감압밸브의 케비테이션 발생을 방지하기 위해서는 돌연확대의 형상을 갖도록 설계하는 것이 타당하다고 판단된다.

• 대한조선학회논문집
• /
• 제39권2호
• /
• pp.1-10
• /
• 2002

선체-프로펠러-타의 상호작용 해석을 반복계산에 의해 수행하였다. 계측된 공칭속도를 입력자료로 하고 보오텍스 링 이론을 이용하여 유효속도를 계산함으로써 선체와 프로펠러사이의 상호작용을 고려하였고, 계산된 유효속도를 입력자료로 하여 프로펠러-타 상호작용을 계산할 수 있는 포텐셜 기저 패널법을 개발하였다. 프로펠러에 의해 타에 유기되는 속도와 반대로 타에 의해 프로펠러에 유기되는 속도는 수렴된 해가 얻어질 때까지 반복 계산하여 타 주위의 정상유동 해석을 수행하였다. 이와 함께 삼성중공업의 대형 캐비테이션 터널에서 L.D.V를 사용하여 프로펠러 및 타 주위의 유동장을 계측하였고 수치계산 결과와 비교하였다. 실선에 설치되고 있는 혼 타주위의 유동장 계산을 위해 gap flow 모델을 적용하였고, 여러 가지 타각에 대한 수치계산을 수행하여 대형캐비테이션 터널에서 계측된 타 표면에서의 압력과 비교하였으며, 계산된 표면 압력 치는 실험 값과 비교적 일치되는 만족스러운 결과를 얻었다.

• Tribology and Lubricants
• /
• 제17권5호
• /
• pp.391-398
• /
• 2001

Two dimensional slow viscous flow around two counter-rotating equal cylinders is investigated based on Stokes'approximation. An exact formal expression of the stream function is obtained by using the bipolar cylinder coordinates and Fourier series expansion. From the stream function obtained, the streamline patterns around the cylinders are shown and the pressure distribution in the flow field is determined. By integrating the stress distributions on the cylinder, the force and the moment exerted on the cylinder are calculated. The flow rate through the gap between the two cylinders is also determined as the distance between two cylinders varies. Special attention is directed to the case of very small distance between two cylinders concerned with the lubrication theory and the minimum pressure is calculated to explain a possible cavitation.

• Tribology and Lubricants
• /
• 제18권6호
• /
• pp.411-417
• /
• 2002

Two dimensional slow viscous flow between a rotating cylinder and a translating plate is investigated using Stokes' approximation. An exact formal expression of the stream function is obtained by using the bipolar cylinder coordinates and Fourier series expansion. From the stream function obtained, the streamline patterns are shown and the pressure distribution in the flow field is determined. By integrating the stress distributions on the cylinder, the farce and the moment exerted on the cylinder are calculated. The flow rate through the gap between the cylinder and the plate is also determined as a function of the distance between the cylinder and the plate. Special attention is directed to the case of very small distance between the cylinder and the plate concerned with the lubrication theory and the minimum pressure is calculated to explain a possible cavitation.

• 대한기계학회논문집B
• /
• 제29권3호
• /
• pp.306-313
• /
• 2005

The performance of a regenerative pump is affected by many parameters, especially blade shape of impeller, leakage flow in the clearance and head losses at the inlet & outlet. An impeller with J-shape blade was designed and 5 times scale up model was tested at similarity conditions to evaluate the performance. Performance variations with clearance change were executed. The amounts of leakage flow through the clearance were estimated using the one-dimensional leakage flow models and analysis. Main leakage flow is generated through the gap between the impeller and casing. The inlet & outlet head losses were also estimated. Such corrections are very important to evaluate the final performance of the impeller and pump. Cavitation test was also performed at 1,200 rpm. NPSH of the regenerative pump was obtained and growth of cavity within blades was visualized.

• 한국유체기계학회 논문집
• /
• 제11권5호
• /
• pp.37-43
• /
• 2008

An inducer is employed in a modern rocket feed system because it allows a turbopump system to operate at a high speed with low inlet pressures so as to minimize the weight and the size of the system. Cavitation performance can be improved by installing an inducer to the pump, enabling to increase the operational speed of the pump. The main purpose of an inducer is to increase the static pressure prior to an impeller to enable the impeller to operate satisfactorily under cavitation environments. In the present study the effects of axial distance between the inducer and the impeller on the performance of the pump were studied using both experimental and computational methods. Two inducers with different axial length were used for the experiments and the pump performances were measured. The experimental results show that the suction performance decreases as the axial gap between the inducer and impeller is increased.

• 대한기계학회:학술대회논문집
• /
• 대한기계학회 2007년도 춘계학술대회B
• /
• pp.3074-3079
• /
• 2007

The conventional control valves have been used at the locations occurring high differential pressure and high temperature which causes cavitation, flashing, severe vibration due to abrupt flow change, and sudden pressure drop. Previous studies concerning control valves focused to prevent damage of valve trim due to the internal leak and low flow rate. The newly designed helical trim of control valve has been installed at the location of high pressure change and high temperature in a power plant, and operated for evaluation. It is confirmed that the new control valve developed in this study generates flow characteristics in comparison with previous helical trim of control valves.

• 대한조선학회 특별논문집
• /
• 대한조선학회 2011년도 특별논문집
• /
• pp.1-4
• /
• 2011

The full spade rudder for the high speed has advantage to prevent gap cavitation of the rudder. DSME has developed the full spade rudder and GL has carried out CFD analysis and FE analysis to confirm strength and fatigue for DSME and Owner. Necessarily, it needs to compare rudder torque & rudder force between CFD, FE analysis and full scale measurement. This report introduces the measurement method and application of strain gauge for measuring the rudder torque and rudder force for the 8,400 TEU container ship.